STOL実験機半截模型風洞試験(半截模型空力要素の特性)

Material type: 文書・図像類

Author: 高橋, 侔ほか

Publisher: 航空宇宙技術研究所

Publication date: 1982-09

Material Format: Digital

Capacity, size, etc.: -

NDC: -

View All

Notes on use

Note (General)：: An investigation has been conducted to determine the aerodynamic characteristics of the aerodynamic elements of an 8％ subsonic jet transport half mode...

Search by Bookstore

Holdings of Libraries in Japan

This page shows libraries in Japan other than the National Diet Library that hold the material.

List of Cooperating Institutions and Databases

Please contact your local library for information on how to use materials or whether it is possible to request materials from the holding libraries.

other

JAXA Repository
Digital
You can check the holdings of institutions and databases with which 学術機関リポジトリデータベース（IRDB）（機関リポジトリ） is linked at the site of 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）.
JAXA Repository

Search by Bookstore

Bibliographic Record

You can check the details of this material, its authority (keywords that refer to materials on the same subject, author's name, etc.), etc.

Digital

Material Type: 文書・図像類
Title: STOL実験機半截模型風洞試験(半截模型空力要素の特性)
Author/Editor: 高橋, 侔
廣末, 健一
宮本, 義人
重見, 仁
岩崎, 昭人
玉置, 元昭
織戸, 満紀雄
森田, 義郎
TAKAHASHI, Hitoshi
HIROSUE, Kenichi
MIYAMOTO, Yoshito
SHIGEMI, Masashi
IWASAKI, Akihito
TAMAKI, Motoaki
ORITO, MAKIO
MORITA, YOSHIO
Author Heading: 高橋, 侔
廣末, 健一
宮本, 義人
重見, 仁
岩崎, 昭人
玉置, 元昭
織戸, 満紀雄
森田, 義郎
TAKAHASHI, Hitoshi
HIROSUE, Kenichi
MIYAMOTO, Yoshito
SHIGEMI, Masashi
IWASAKI, Akihito
TAMAKI, Motoaki
ORITO, MAKIO
MORITA, YOSHIO
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1982-09
Publication Date (W3CDTF): 1982-09
Alternative Title: Wind Tunnel Investigation of an Upper Surface Blown-Flap Half Model of the NAL STOL Research Aircraft
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-734
No. or year of volume/issue: 734
Volume: 734
Pages: 32-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: jpn
Target Audience: 一般
Note (General): An investigation has been conducted to determine the aerodynamic characteristics of the aerodynamic elements of an 8％ subsonic jet transport half model with an upper surface blowing flap system that would augment lift. Wind tunnel tests of leading edge and trailing edge high lift devices were conducted. After investigating those wind tunnel test data, some results were obtained. The set up angles of outer leading edge slats which were divided into three parts were all fixed at 40 degrees. It was determined that the USB flap was a hinged 40-70 type Forward-Main flap and that the inner leading edge had no device because any inner leading edge high lift devices were less effective in augmenting lift. Many data obtained in the wind tunnel tests were offered for the design of the NAL STOL Research Aircraft.
資料番号: NALTR0734000
レポート番号: NAL TR-734
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44991&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44991&item_no=1&attribute_id=31&file_no=1
Access Restrictions: 限定公開
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ